parameters_module Module


Uses

  • module~~parameters_module~~UsesGraph module~parameters_module parameters_module fortran_astrodynamics_toolkit fortran_astrodynamics_toolkit module~parameters_module->fortran_astrodynamics_toolkit module~halo_kinds_module halo_kinds_module module~parameters_module->module~halo_kinds_module iso_fortran_env iso_fortran_env module~halo_kinds_module->iso_fortran_env

Used by

  • module~~parameters_module~~UsedByGraph module~parameters_module parameters_module module~config_file_module config_file_module module~config_file_module->module~parameters_module module~halo_module halo_module module~halo_module->module~parameters_module module~halo_module->module~config_file_module module~halo_utilities_module halo_utilities_module module~halo_module->module~halo_utilities_module module~halo_utilities_module->module~parameters_module proc~halo_solver_main halo_solver_main proc~halo_solver_main->module~parameters_module

Variables

Type Visibility Attributes Name Initial
integer, public, parameter :: n_eoms = 6

size of EOM derivative vector [x,y,z,vx,vy,vz]
real(kind=wp), public :: mu_earth = 3.9860043543609593E+05_wp

real(kind=wp), public :: mu_moon = 4.9028000661637961E+03_wp

real(kind=wp), public :: mu_sun = 1.3271244004193938E+11_wp

real(kind=wp), public :: mu_jupiter = 1.266865349218008E+08_wp

-- from https://naif.jpl.nasa.gov/pub/naif/generic_kernels/pck/gm_de431.tpc
real(kind=wp), public :: rad_moon = 1737.4_wp

radius of the Moon
real(kind=wp), public :: rad_sun = 695700.0_wp

sun radius (km)
real(kind=wp), public :: rad_earth = 6378.0_wp

earth radius (km)
integer, public :: maxnum = 10000

integrator max steps
integer, public :: grav_n = 8

max grav degree
integer, public :: grav_m = 8

max grav order
integer, public :: grav_frame = 1

1: iau_moon, 2: moon_pa (splined)
real(kind=wp), public, dimension(:), allocatable :: xscale_x0
real(kind=wp), public, dimension(:), allocatable :: fscale_xf
real(kind=wp), public :: fscale_rdot = 1.0_wp

scale value for the rdot=0 constraint
logical, public :: use_battin_gravity = .false.

use Battin gravity formulation
character(len=:), public, allocatable :: mkspk_path

for mkspk: path to mkspk executable. e.g. kernel/mkspk
integer, public :: object_id = -50000

for mkspk: OBJECT_ID
character(len=:), public, allocatable :: object_name

for mkspk: OBJECT_NAME
character(len=:), public, allocatable :: leapseconds_file

for mkspk: LEAPSECONDS_FILE
character(len=:), public, allocatable :: segment_id

for mkspk: SEGMENT_ID
integer, public :: polynom_degree = 9

for mkspk: POLYNOM_DEGREE
integer, public :: output_spk_type = 9

for mkspk: OUTPUT_SPK_TYPE
real(kind=wp), public :: min_export_time_step = 0.0_wp

minimum time (sec) step for exporting to mkspk file [to try and avoid spice interpolation issues for very small time steps]

Derived Types

type, public ::  patch_point

a CR3BP Halo state, to be used as an initial guess for the full force model.

Components

Type Visibility Attributes Name Initial
real(kind=wp), public :: t = zero

Time from Periapse (days from periapsis)
real(kind=wp), public, dimension(6) :: rv = zero

Rx (km) Ry (km) Rz (km) Vx (km/s) Vy (km/s) Vz (km/s) [moon-centered earth-moon rotating frame]